name = Su-30
manufacturer = Sukhoi
caption = Indian Air Force Su-30K landing with an airbrake.
first flight = 1989
introduction = 1996
status = Operational
primary user =
Russian Air Force
more users =
Indian Air Force Algerian Air ForcePLA Air Force
number built =
unit cost = US$33-$45 million
developed from =
variants with their own articles =
Sukhoi Su-30MKI Sukhoi Su-30MKK
The Sukhoi Su-30 (
NATO reporting name"Flanker-C") is an agile military aircraftdeveloped by Russia's Sukhoi Aviation Corporationand introduced into operational service in 1996. It is a multi-role strike fighter that can perform both air superiority and ground attack missions.
The aircraft is a modernized version of the Su-27UB and has several variants. The Su-30K and Su-30MK series have had commercial success. The variants are manufactured by competing organizations:
KNAAPOand the IRKUT Corporation, both of which come under the Sukhoi group's umbrella. KNAAPO manufactures the Su-30MKK and the Su-30MK2, which were designed for and sold to China. Irkut makes the long-range, multirole Su-30MK series. The series includes the Su-30MKI developed for the Indian Air Forceand its derivatives, the MKM, MKA and MKV for Malaysia, Algeriaand Venezuelarespectively.
Su-27PU long-range interceptor
While the original Su-27 had good range, it still did not have enough for certain air-defense tasks required by the PVO Strany ("PVO" being short for "Protivo-Vozdushnaya Oborona" — "Air Defense") whose requirements spanned the need to cover the vast expanse of the Soviet Union. Hence, development began in 1986 on the Su-27PU, an improved-capability variant of the Su-27 capable of serving as a long-range interceptor or airborne command post. The two-seat Su-27UB combat trainer was selected as the basis for the Su-27PU, because it had the performance of a single-seat Su-27 and long-range missions require two crewmen. A "proof-of-concept" demonstrator flew
6 June 1987, and this success led to the kick-off of development work on two Su-27PU prototypes. The first Su-27PU flew at Irkutsk on 31 December 1989, and the first of three pre-series models flew in 14 April 1992.
* To adapt the Su-27UB to its new role, the aircraft was fitted with a retractable
in-flight refuelingprobe to increase range; the probe is offset to the left side of the nose and, to accommodate it, the IRSTwas offset to the right.
* The aircraft's
avionicswere changed, fitting special communications and guidance equipment to command formation flights of single-seat Su-27 interceptors. The rear cockpit received a large CRT display which provides the formation leader with tactical information regarding targets and interceptors. The navigation and fly-by-wiresystems were also upgraded. It was fitted with an updated NIIP N001 radar, providing some ability for air-to-ground attack and to track and engage multiple aerial targets simultaneously.
Sukhoi offered the Su-27PU to be used as a "fighter controller", a sort of mini-AWACS, with the back-seater using the radar and data links to control other fighters. However, the PVO was not interested in buying the Su-27PU. All five Su-27PUs, with the new designation of "Su-30", ended up in PVO service in the training role. Deliveries to the 54th Interceptor Air Regiment at the advanced training base at Savostleyka began in 1996.
It is fitted with an airbrake behind the cockpit.
According to a German Technical survey magazine, the Su-30MKI (Indian version) is the best combat fighter-bomber aircraft in the world.Fact|date=September 2008
A Su-30M two-seat multirole variant was proposed for Russian use and a few may have been built in the mid-1990s for evaluation.
* Sukhoi proposed an export variant, Su-30MK, where "MK" stood for "Modernizirovannyi Kommercheskiy" (Modernized Commercial). Sukhoi displayed a Su-30MK demonstrator at the
Paris Air Showin 1993.
* A much more optimized Su-30MK demonstrator, rebuilt from the first production Su-27PU, was displayed in 1994.
Highly flexible multi-role fighter
The Su-30MK is capable of accomplishing a wide variety of combat missions at significant distances from the home base, in any weather conditions and in severe
jammingenvironment, both by day and by night.
This multirole aircraft is adequately fitted for the entire spectrum of tactical and operational combat employment scenarios, varying from counter-air tasks (ie. gaining
air superiority, air defense, air patrol and escort) to ground attack, suppression of enemy air defenses, air interdiction, close air supportand maritime attack. Additionally, the Su-30MK can perform ECCMand early warning tasks, as well as exercise command-and-control over a group of aerial combat assets performing joint missions.
Angle of attack
The Su-30MK's aerodynamic configuration is an unstable-in-longitude triplane (see
relaxed stability). To increase lifting effectiveness and enhance maneuverability of the aircraft, canards are installed. They are deflected automatically to ensure controlled flight at high angles-of-attack. Canards, however, are installed only in some Su-30 variants like the Su-30MKI.
Pugachev's Cobra maneuver
The integrated aerodynamic configuration, combined with the
thrust vectoringcontrol ability, results in unprecedented maneuverability and unique takeoff and landing characteristics. Equipped with a digital fly-by-wire system, the Su-30MK is able to perform some very advanced maneuvers. They include the well-known Pugachev's Cobraand the Bell. While performing a somersault maneuver the aircraft makes 360-degree turn in the pitch plane without any loss of altitude. In the Controlled Flat Spin maneuver the aircraft performs several full turns in the horizontal plane, with zero forward speed, virtually on the spot.
The aircraft's power plant incorporates two Saturn
AL-31FP afterburning low-bypass turbofanengines. A total afterburning thrust of 25,000 kgf(245 kN) ensures Mach2 horizontal flight speed, 1,350 km/h speed at low altitude, and a 230 m/s climbing rate.
With a normal fuel reserve of 5,270 kg, the Su-30MK is capable of performing a 4.5-hour combat mission with a range of 3,000 km. An in-flight refueling system increases the flight duration up to 10 hours with a range of 8,000 km at
cruise altitudes of 11 to 13 km.
The long range significantly increases deployment options. The missions vary from prolonged patrols and escorts to long-range intercepts and air-to-ground strikes.
Diagonally 2D thrust vectoring control
Differential ±15-degree deflection of the engines' asymmetric nozzles (with turn axes positioned at 32-deg angle to each other) enables pitch/yaw thrust vectoring control. Depending on the maneuver to be performed, nozzles deflections can be synchronized with or differ from the deflections of horizontal tail planes.
A two-member crew configuration contributes significantly to enhanced combat capabilities, due to rational distribution of workload between crewmembers. While the first pilot flies the aircraft, controls weapons and performs maneuvering dogfight, the co-pilot employs
BVRair-to-air and air-to-ground guided weapons in long-range engagements, monitors tactical environment to ensure situational awareness, and performs command-and-control tasks in group missions.
Radar: Either a N001VEor Phazotron N010 Zhuk-27 or an N011M BARSpulse Doppler passive electronically scanned arrayradar. Capable of detecting and tracking up to 15 air targets, while concurrently attacking four of them. The N011M BARS radar (featuring a 20- m(65.6 ft) resolution) ensures detection of large sea-surface targets at a distance of up to 400 km (248.5 mi), and small-size ones at a distance of up to 120 km (74.5 mi).
* Other avionics include an integrated optronic sighting-and-navigation system with a laser gyro navigation system; helmet-mounted displays, a head-up-display, multi-function color
LCDs with image mixing ability; and a GPSsystem ( GLONASS/ NAVSTARcompatible).
* IR and
lasersighting pods to detect and engage small-size ground targets are available for installation. The aircraft is provided with an ECCM facility intended to subvert hostile electronic and electro-optical countermeasures.
* The aircraft features
autopilotability at all flight stages including low-altitude flight in terrain-following mode, and individual and group combat employment against air and ground/sea-surface targets. Automatic control system interconnected with the navigation system ensures route flight, target approach, recovery to airfield and landing approach in automatic mode.
*A standard Su-30K is estimated at US$34 million which is more than double the cost of an F-16A Fighting Falcon. [ [http://www.fas.org/man/dod-101/sys/ac/row/su-30.htm Su-30 ] ]
Su-30MKKvariant is estimated at US$53 million.
;Su-27PU:Long range interceptor based on two-seater Su-27UB trainer. Later renamed Su-30.;Su-30:Testbed fighter with canards added.;Su-30K:Commercial version of the basic Su-30. 50 units sold to India and later upgraded to Su-30MKI.;Su-30KI:Sukhoi proposal for upgrading Russian AF single seat Su-27S. Also proposed export version for Indonesia, 24 was ordered but subsequently cancelled due to the ASEAN economic crisis [http://www.milavia.net/aircraft/su-27/su-27_ops.htm MILAVIA - Sukhoi Su-27 'Flanker' - Operator List ] ] , only single seat in Su-30 family.;Su-30KN:Upgrade for operational two-seat fighters, the Su-27UB, Su-30 and Su-30K.;Su-30M:Basically an upgraded Su-27PU, first real multi-role aircraft in Su-27 family.;Su-30MK:The commercial version of Su-30M first revealed in 1993.;Su-30M2:Upgraded Su-30MK with canards and TVC.;Su-30MKI:MKI stands for "Modernizirovannyi Kommercheskiy Indiski" meaning "Modernized Commercial India". Jointly-developed with
India's Hindustan Aeronautics Limitedfor the Indian Air Force. Includes Thrust VectoringControl (TVC) and canards. Equipped with a multi-national avionics complex sourced from Israel, India, Russia and France. [ [http://www.aircraftinaction.co.uk/2007/Waddington.htm SU30MKI] ] ;Su-30MKK:Export version for China.;Su-30MKM:Based on the MKI, a highly specialised version for Royal Malaysian Air Forcewith the same platform but a French, South African and Russian combination of avionics. It will feature head-up displays (HUD), navigational forward-looking IR system (NAVFLIR) and Damocles Laser Designation pod (LDP) from Thales Group of France, MAW-300 missile approach warning sensor (MAWS) and laser warning sensor (LWS) from SAAB AVITRONICS (South Africa) [http://www.armada.ch/07-6/02_Aircraft_Self_Protection.pdf] , as well as the Russian NIIP N011M BARS PESA radar, electronic warfare (EW) system, optical-location system (OLS) and a glass cockpit. [http://www.irkut.com/en/news/press_release_archives/index.php?id48=252] ;Su-30MKV:Export version for Venezuela is most likely to be similar to the Su-30MK2. This is based on the presence of two such demonstrator models (No. 0460 and No. 1259) from the KNAAPO facility that took part in July 2006 national day parade in Caracas. The latest news confirm that the Su-30 purchased by Venezuela are indeed Su-30MK2.;Su-30MK2:Su-30MKK with upgraded electronics that enabled support for anti-ship missiles;Su-30MK2V:Su-30MK2 variant for Vietnam with minor modifications.;Su-30MK3:Su-30MKK with Zhuk MSE radar and Support for Kh-59MK anti-ship missile.;Su-30MKA:Highly specialised version for Algeria is similar to the MKI, but will principally be equipped with French and Russian avionics. It will feature head-up and multifunction displays from the Thales Groupand Sagemof France.
Algerian Air Forceoperates 44 Su-30MKA version.Fact|date=July 2008;PRC
People's Liberation Army Air Forceoperates 76 Su-30MKK (Russian: "Modernizirovannyi Kommercheskiy Kitaya"; Modernized Commercial China). The PLAAF was already operating the Su-27. The first batch of 38 were delivered between December 20, 2000and the end of 2001. The second batch of 38 were ordered in 2001 and thought to have been delivered by 2003.
People's Liberation Army Naval Air Forceoperates 24 Su-30MK2. They were ordered in January 2003 and delivered by August 2004.;IND
* Indian Air Force, after years of negotiations, decided to purchase 50 Su-30 aircraft and acquired the licence from Sukhoi and Russia to manufacture an additional 140 Su-30MKI aircraft. India is expected to eventually acquire a total of 230 aircraft. Currently 116 Sukhoi-30MKI are in service.;IDN
Indonesian Air Forceoperates 2 Su-27SK & 2 Su-30MK aircraft. [ [http://mdb.cast.ru/mdb/2-2005/am/rusmilitary/ Moscow Defense Brief] ] and signed a deal in 2006 to buy 3 Su-27SKM and 3 Su-30MK2 with a possible follow up order of 16. ;MYS
Royal Malaysian Air Forceafter a close visit to India's Su-30MKI, signed a deal to purchase 18 of Su-30MKM (M for Malaysia) in May 2003. The first 2 Su-30MKMs were formally handed over in Irkutsk on 23 May 2007, later arrived in Gong Kedakairbase on 21 June. Full squadron of 18 aircraft will be operational by the end of 2008. As part of the deal, the Russians will send a Malaysian astronaut to the ISS.;RUS
Russian Air ForceOperates at least 19 which are all in service with the Russian Air Force VVS ;VEN
Venezuelan Air Forceand the government of Venezuela on 14 June 2006, announced the purchase of 24 units of the Su-30MK2 aircraft. The first two Su-30MK2s arrived in the first week of December 2006 while another 8 were commissioned during 2007, fourteen more units have arrived in 2008 with the last 4 being delivered in August. [ Air Forces Monthly, August issue.] [ [http://en.rian.ru/world/20080804/115619889.html RIA Novosti - World - Chavez warns U.S. after getting Russian warplanes] ] ;VNM:
Vietnam People's Air Forceoperates 15 Su-30MK2V version.
plane or copter?=plane
jet or prop?=jet
ref=KNAAPO Su-30MK page, [ [http://www.knaapo.ru/eng/products/military/su30mk.wbp Sukhoi Su-30MK] , KNAAPO.] Sukhoi Su-30MK page, [ [http://www.sukhoi.org/eng/planes/military/su30mk/lth/ Su-30MK Aircraft performance page] , Sukhoi.] Gordon and Davison [Gordon and Davison 2006, pp. 92, 95-96.]
length main=21.935 m
length alt=72.97 ft
span main=14.7 m
span alt=48.2 ft
height main=6.36 m
height alt=20.85 ft
area main=62.0 m²
area alt=667 ft²
empty weight main=17,700 kg
empty weight alt=39,021 lb
loaded weight main=24,900 kg
loaded weight alt=54,900 lb
useful load main=
useful load alt=
max takeoff weight main=34,500 kg
max takeoff weight alt=76,060 lb
engine (jet)= AL-31FL
type of jet= low-bypass turbofans
number of jets= 2
thrust main= 7,600 kgf
thrust alt=74.5 kN, 16,750 lbf
afterburning thrust main=12,500 kgf
afterburning thrust alt=122.58 kN, 27,560 lbf
max speed main=Mach 2.0
max speed alt=2,120 km/h, 1,320 mph
cruise speed main=
cruise speed alt=
range main=3,000 km
range alt=1,620 nmi
range more=at altitude
ferry range main=
ferry range alt=
ferry range more=
ceiling main=17,300 m
ceiling alt=56,800 ft
climb rate main=230 m/s
climb rate alt=45,275 ft/min
loading main= 401 kg/m²
loading alt= 82.3 lb/ft²
armament=The Su-27PU had 8 hardpoints for its weapon load, whereas the Su-30MK's combat load is mounted on 12
hardpoints: 2 wingtip AAM launch rails, 3 pylons under each wing, 1 pylon under each engine nacelle, and 2 pylons in tandem in the "arch" between the engines. All versions can carry up to 8 tonnes of external stores.
* Guns: 1×
GSh-30-1gun (30 mm caliber, 150 rounds)
* AAMs: 6× R-27ER1 (AA-10C), 2× R-27ET1 (AA-10D), 6× R-73E (AA-11), 6× R-77 RVV-AE(AA-12)
* ASMs: 6× Kh-31P/Kh-31A anti-radar missiles, 6× Kh-29T/L laser guided missiles, 2× Kh-59ME
* Aerial bombs: 6× KAB 500KR, 3× KAB-1500KR, 8× FAB-500T, 28× OFAB-250-270
Incidents and accidents
June 12, 1999: Paris Air Show ( [http://www.youtube.com/watch?v=Qd0eV95ipQk Video] )
June 10, 2006: Le Bourget, Paris Air Show, France, a Russian Su-30MK crashed - both pilots ejected safely and no one was hurt on the ground. [http://www.aeronautics.ru/nws001/msnbc001.htm]
F-15E Strike Eagle
List of fighter aircraft
List of military aircraft of the Soviet Union and the CIS
4th generation jet fighter
*Gordon, Yefim and Peter Davison. "Sukhoi Su-27 Flanker", Specialty Press, 2006. ISBN 978-1-58007-091-1.
* [http://www.sukhoi.org/eng/planes/military/su30mk/ Su-30MK page on Sukhoi.org]
* [http://www.fas.org/man/dod-101/sys/ac/row/su-30.htm Su-30 page on FAS.org]
* [http://www.globalsecurity.org/military/world/russia/su-30.htm Su-30 page on GlobalSecurity.org]
* [http://www.milavia.net/aircraft/su-30/su-30.htm Su-30 page on Milavia.net]
* [http://www.airforce-technology.com/projects/su_30mk Su-30MK page on Airforce-Technology.com]
* [http://www.ausairpower.net/APA-Flanker.html Sukhoi Flankers - The Shifting Balance of Regional Air Power]
* [http://www.vectorsite.net/avsu27.html Su-27 Series at Greg Goebel's AIR VECTORS]
* [http://www.aeronautics.ru/archive/vvs/su30-01.htm Su-30 page on Veniks Aviation]
* [http://www.sci.fi/~fta/Su-30.htm Su-30 page on Fighter Tactics Academy site]
* [http://www.ausairpower.net/TE-Flankers-Aug03.pdf Asia's Advanced Flankers on ausairpower.net]
* [http://www.flightlevel350.com/aviation_videos.php?airplane=Sukhoi+Su-30 Sukhoi Su-30 Videos]
* [http://youtube.com/watch?v=YwCDP8SJCIk Video on YouTube]
* [http://www.patricksaviation.com/videos/search/?q=su-30 Su-30 Videos]
* [http://www.airliners.net/open.file/1300906/L/ Malaysian SU-30MKM]
* [http://www.mars.slupsk.pl/fort/sukhoi/default.htm Sukhoi Su-30 story in colours]
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